One question per week – questions related to stress corrosion
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This post was last edited by lanye55 on 2009-9-10 08:35. What is the concept of stress corrosion cracking? Which media can easily cause stress corrosion cracking in austenitic stainless steels? Are there any effective and practical pre-treatment methods to prevent stress corrosion cracking in stainless steel? By reviewing the old, we can gain new insights; I hope everyone will participate actively, learning together through interaction and improving together!Material | Environmental medium
Carbon steel and low-alloy steel | Sodium hydroxide solution, nitrate solution, acidic hydrogen sulfide solution, seawater, marine or industrial atmospheres
Stainless steel | Acidic oxide solutions, sodium chloride-hydrogen peroxide solution, hydrogen sulfide, seawater, sodium hydroxide-hydrogen sulfide solution
High-strength steel | Rainwater, seawater, hydrogen sulfide solution, sodium chloride aqueous solution
Nickel-based alloys | Hot concentrated sodium hydroxide solution, hydrogen fluoride vapor and solutions
Aluminum alloys | Sodium chloride-hydrogen peroxide solution, sodium chloride aqueous solution, water vapor, seawater
Copper alloys | Ammonia vapor and solutions, aqueous solutions containing ammonium ions
Magnesium alloys | Sodium chloride-potassium chromate solution
Titanium alloys | Seawater, methanol, salt solutions
Monel | Hydrofluoric acid, fluorosilicic acid
The characteristics of stress corrosion fracture mentioned above can help us determine whether a fracture incident is due to stress corrosion. However, it is necessary to consider various factors as a whole; one should not draw conclusions simply based on a single characteristic. 2. Mechanism of stress corrosion The process of stress corrosion fracture also involves crack formation and growth, and can be divided into the following three stages: (1) Incubation stage: This is the period prior to crack formation; during this time, corrosion pits are formed to serve as the nuclei for cracks. When there are defects on the surface of the component that can act as sites for stress corrosion cracks (such as grain boundaries, twin boundaries, inclusions, etc.), there is no incubation stage – only a crack propagation stage. (2) Sub-stable crack propagation stage: Under the combined effect of stress and the environmental medium, the crack propagates slowly. (3) Crack instability propagation stage: Mechanical fracture that occurs once the crack reaches a critical size. There are various theories regarding the formation and propagation of cracks under the combined action of stress and environmental media. The more widely accepted theories to date include the anodic dissolution mechanism, in which anodic dissolution serves as the controlling process for fracture, and the hydrogen embrittlement mechanism, in which cathodic hydrogen absorption is the controlling process (the hydrogen embrittlement mechanism will be discussed later). It is important to note here the relationship between stress corrosion cracking (SCC) and hydrogen-induced cracking (HIC). Logically, they are “intersecting,” meaning that part of their content overlaps. If SCC is primarily caused by hydrogen evolution from the corroded cathode process, then this SCC is also HIC ; If SCC is primarily caused by the anodic dissolution process, then such SCC is not HIC. Under normal circumstances, cathodic polarization with an applied potential can be used to determine the SCC mechanism; that is, if accelerated fracture occurs, it belongs to the HIC mechanism ; If it slows down or is suppressed, it belongs to the anodic dissolution mechanism. This causes the anode potential to drop, accelerating the dissolution of the anode metal; cracks then gradually extend deeper, as shown in Figure 7-2. The aforementioned mechanism of anode dissolution actually involves four stages: sliding, film rupture, anode dissolution, and re-passivation. In the case of stress corrosion cracking that occurs through the grain, the breakdown of the protective film is caused by the formation of slip steps in local regions under stress. In the case of cracking that occurs along the grain boundaries, segregation at those boundaries or the precipitation of continuous phases leads to the formation of steps on the surface formed by individual grains, which in turn causes the breakdown of the surface protective film, ultimately resulting in stress corrosion cracking. For example, the stress corrosion cracking in martensitic stainless steel occurs mainly along grain boundaries, but when tempered below 455°C, it takes place through the grain boundaries. 3. Characteristics of stress corrosion fracture surfaces: The macroscopic morphology of stress corrosion fracture surfaces is quite similar to that of fatigue fracture surfaces, and it also consists of three zones: (1) the fracture initiation zone. It is generally caused by local corrosion or other types of cracks, such as pitting corrosion and crevice corrosion. These source cracks can be welding cracks, fatigue cracks, heat treatment cracks, etc. Stress corrosion microcracks originate from the surface and are discontinuous; they are characterized by numerous branches and a sharp, dendritic shape. (2) The metastable growth zone of stress corrosion cracks. This is a process of slow propagation of stress corrosion cracks, which is a result of the interaction between the material’s microstructure, stress, and environmental conditions. Macroscopically, this process is characterized by brittleness; even in Cr-Ni-based austenitic stainless steels with high plasticity, the cracks propagate along certain crystallographic directions of the material (such as cleavage planes), resulting in a black or grayish-black appearance. These corrosion products are quite important in the analysis of subsequent fracture incidents. (3) Final interruption zone. It is a rapid breakage zone or tearing zone, reflecting the properties of the matrix material. The microcracks in stress corrosion exhibit branching, indicating that during stress corrosion, a primary crack expands more rapidly while the other branch cracks expand more slowly. Based on this characteristic, stress corrosion can be distinguished from stress fatigue, intergranular corrosion, and other forms of fracture. The microstructure of stress corrosion fracture exhibits very distinct features: corrosion pits, corrosion products, and mud pattern textures. The mud pattern consists of linear cracks distributed on a flat surface (similar to the appearance of a dried riverbed); it is a coating formed by corrosion products. During transgranular fracture, the fracture surfaces observed under an electron microscope present as flat grooves (with a depth greater than the width), fan-shaped patterns, steps, and river-like patterns. The grooved areas are the result of the combined effect of stress and corrosive agents, while the fan-shaped patterns and steps arise from the connection of stress corrosion cracks on different planes; it is merely the difference in observation direction that results in varying fracture patterns. In short, the fracture characteristics of stress corrosion are quite complex. It is related to the crystal structure of the material, its mechanical properties, alloy composition, heat treatment condition, environmental atmosphere, as well as temperature and pressure conditions. It can exhibit a brittle fracture pattern, and a ductile fracture pattern can sometimes be observed as well; the mode of fracture can be intergranular or transgranular. For example, under normal conditions, low-carbon steel, low-alloy steel, aluminum alloys, and α-brass undergo grain-edge fracture, whereas β-brass and austenitic stainless steels exposed to chlorides generally experience transgranular fracture. Based on the aforementioned mechanisms and conditions that lead to stress corrosion, the main method of preventing stress corrosion cracking is to select materials appropriately; that is, materials with low sensitivity to stress corrosion should be chosen for components subjected to certain stresses and operating conditions. For example, brass is highly sensitive to stress corrosion cracking in the presence of ammonia, so copper alloys should be avoided as much as possible in components that come into contact with ammonia ; Secondly, reducing or eliminating residual tensile stress in the parts can lower their susceptibility to SCC; this is achieved by minimizing stress concentrations in the parts during design, ensuring uniform heating and cooling during manufacturing processes, and using annealing processes when necessary to eliminate stress. By counteracting or partially offsetting the effects of external tensile stress, it is possible to help prevent SCC ; Furthermore, improving the medium conditions can help prevent stress corrosion by adding corrosion inhibitors or protective coatings, as well as by reducing and eliminating harmful chemical ions that promote stress corrosion; stress corrosion can be avoided through such changes in the medium conditions ; For example, reducing the chloride ion content in cooling water and steam water through water purification is highly effective in preventing stress corrosion cracking in austenitic stainless steels; therefore, improving the design of metal components to prevent the accumulation of corrosive agents is an important measure for suppressing SCC. Finally, from the perspective of electrochemical protection, cathodic protection can also be used to prevent stress corrosion, as cathodic polarization can reduce the crack propagation rate; however, it should be noted that cathodic protection cannot be applied to high-strength steels or other materials sensitive to hydrogen embrittlement.